Most spaceborne scientific experiment
applications require a microgravity
environment. The current high-precision accelerometers used for the
spaceborne vibration isolation system generally have a noise floor
of sub-μg/√Hz, which cannot meet the demand of higher-level
microgravity measurements. This article introduces a micro-electromechanical
system (MEMS) acceleration sensor that has a noise floor of 2–5
ng/√Hz and an input range of more than ±2 mg. Its three-component
version, the MEMS microgravity measurement module (MEMS-M3), is designed to measure accelerations in the space microgravity
environment and might be used in the active vibration isolation system
for higher-level microgravity scientific experiments in the future.
The MEMS-M3 has a volume of 105 × 90 × 115 mm3, a weight of 1.2 kg, and power consumption of 3 W. The performance
of the MEMS-M3 has been characterized on the ground and
a series of preflight reliability experiments have been conducted.
Then, the MEMS-M3 installed inside the test spacecraft
has been carried by the Long March 5B rocket (CZ-5B) to the low Earth
orbit at 10:00 on May 5, 2020, and returned to Earth ground at 5:00
on May 8, 2020, both in UTC time. During the on-orbit period, the
MEMS-M3 has been switched on for 11 h. After data processing,
the transient, periodic, and steady accelerations can be observed
by the MEMS-M3 and a much noisier shelf product IMU STIM300,
verifying the functionality of the MEMS-M3. Apart from
application in active vibration isolation systems for spaceborne scientific
experiments, it can also be used for drag-free control of satellites
and other space applications.